Materials 5: Polymers, ceramics and composites Flashcards

1
Q

What properties can be obtained from an impact test?

A

1) The amount of energy absorbed by a material during fracture. The energy required to fail a material is related to the area under the true stress-true strain characteristics. Metals with high strength and high ductility have good toughness while ceramics and some composites have poor toughness due to their poor ductility despite having high strength. 2) Impact testing can be used to determine the transition temperature of materials; i.e. the temperature at which the material changes from brittle (low temperature) to ductile (high temperature) failure. Hence if a material is likely to be subjected to impact loading while in-service a material should be selected which has a transition temperature well below its in-service temperature minimum.

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2
Q

How is a typical fracture toughness test performed?

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 All materials contain flaws to one degree or another - these occur during synthesis, processing, abuse and in-service use.  These flaws can lead to stress concentrations or weaknesses within the material depending on the number, size and geometry of these ‘defects’.  Fracture toughness can be used to determine the influence of these flaws on the material to withstand applied loads A typical test to determine fracture toughness of a material is to apply a stress to a sample, which has a known flaw in terms of size and geometry, inserted in it. The applied stress is intensified by the presence of the flaw, which acts as a stress raiser

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3
Q

What factors allow materials to resist crack growth?

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 Larger flaws reduce the load bearing stress in a material. Therefore during manufacture impurities are filtered from liquid metals and hot pressing of ceramic components reduces the flaw size and hence enhances fracture toughness.  Increased ductility increases fracture toughness. Increasing the strength of a metal decreases ductility and hence reduces fracture toughness i.e. there is a trade-off in properties. Brittle materials such as ceramics and some polymers have much lower fracture toughness than many metals.  Thickness of materials influences the fracture toughness with thicker more rigid materials having lower fracture toughness than thin materials.  The rate of load application, e.g. impact testing, reduces the fracture toughness of materials.  Increase of temperature increases fracture toughness .  A small grain size improves fracture toughness. More point defects (especially large) and dislocations reduce fracture toughness. Hence a fine-grained ceramic material helps to improve resistance to crack propagation.

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4
Q

Describe how a fatigue test is performed?

A

 Components are often subjected to repeated application of stress below the yield strength of the material.  After a significantly large number of cycles failure can result, despite the loading being well below the yield strength.  E.g. Wings of an aircraft where the structural components are subjected to cyclical loading. This cyclical stress occurs in different components due to rotation, flexure or even vibration.  This mode of failure is known as fatigue. Fatigue Testing:  A specified mean load (which may be zero) and an alternating load are applied to a specimen and the number of cycles required to produce failure (fatigue life) is recorded.  Generally, the test is repeated with identical specimens and various fluctuating loads.  Loads may be applied axially, in torsion, or in flexure.

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5
Q

What are the three stages of fatigue in materials?

A
  1. Initially a tiny crack commences at a surface after continual cyclical loading. 2. The crack then gradually propagates as the load cycling continues. 3. Finally a sudden and catastrophic failure occurs when the remaining cross-section of the material is insufficient to carry the applied load.
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6
Q

What type of polymer material might you select for the following applications? Surgeons glove A pulley

A

SOLUTION a) Surgeons glove  The glove must be capable of stretching a great deal in order to slip onto the surgeons hand, yet it must conform tightly to the hand to permit the maximum sensation of touch during surgery.  A material that undergoes a large amount of elastic strain – particularly with relatively little applied stress – might be appropriate.  This requirement describes an elastomer. b) A pulley:  The pulley must be subjected to some stress and wear as a belt passes over it.  A relatively strong, rigid, hard material is required to prevent wear.  A thermosetting polymer might be most appropriate.

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7
Q

An amorphous polymer is pulled in a tensile test. After a sufficient stress is applied, necking is observed to begin on the gauge length. However, the neck disappears as the stress continues to increase. Explain this behaviour.

A

 Normally, when necking begins, the smaller cross-sectional area increases the stress at the neck and necking is accelerated.  However, during this tensile test, the chains in the amorphous structure are straightened out and the polymer becomes more crystalline.  When necking begins, the chains at the neck align and the polymer is locally strengthened sufficiently to resist further deformation at that location.  Consequently, the remainder of the polymer, rather than the necked region, continues to deform until the neck disappears.

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8
Q

Describe giving examples, what factors affect the inherent viscosity of a polymeric material.

A

• Molecular Architecture • Molecular chain length • Molecular weight distribution • Additive system employed

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9
Q

Describe TWO methods for the determination of flow behaviour in a polymer. What advantages and disadvantages do these methods have in a polymer manufacturing environment?

A

1) Capillary Rheometer The basic principle is that a thermoplastic sample (originally in the shape of granules, powder or flakes) is made fluid by heating and forced to flow out of a cylinder through a capillary die. The measured quantity is normally the generated pressure under steady state conditions. A flow curve is the typical output, obtained by interpolation of several experimental data. 2) Melt Flow Indexer It is defined as the mass of polymer, in grams, flowing in ten minutes through a capillary of a specific diameter and length by a pressure applied via prescribed alternative gravimetric weights for alternative prescribed temperatures

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10
Q

Identify the parts of a thermoplastic extruder

A
  1. Motor and gearbox 2. Hopper 3. Water cooling system 4. Heater bands 5. Thermocouples 6. Screw 7. Screen pack 8. Breaker plate 9. Adapter zone 10. Die
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11
Q

(a) Describe the polymer manufacturing process of extrusion. (b) Identify the typical properties which can be determined using thermo-analytical techniques and why these are important?

A

(a). The extruder is essentially a screw conveyor: Carries cold plastic granules (or powder) forward Compacts them under pressure at high temperature Feeds the material forward into the form shaping die as a uniform and homogeneous melt (b) Thermo-Analysis (studying polymer properties as they change with temperature)  Differential scanning calorimetry (DSC) Chemical changes Melt  Thermogravimetric analysis (TGA) Physical changes: Weight loss and gain Moisture storage Degradation  Thermomechanical analysis(TMA) Expansion/contraction in the mould Mould design etc By carrying out these types of tests, you are attempting to simulate manufacturing processes. Determine times polymer can be in the barrel or mould before changes take place. Differences in off-line / industrial techniques. Helps reduce development time for new materials/products

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12
Q

What factors of the in-coming raw polymeric material need to be assessed for quality control purposes?

A

To gain the most comprehensive understanding of the raw material, the following should be assessed:  Flow characterisation under simulated processing conditions  Thermal response  Granule size variation  Residue content, e.g. By ashing or TGA Note that the cost implications of this can be quite significant.

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13
Q

Describe with the aid of diagrams the three zones in an extruder and the importance of each for the manufacture of polymeric products.

A
  1. Feed Zone • Feeds solids forward • Packs material • Melt film begins to form (gel point) 2. Compression Zone • Flight depth decreases • Pressure increases • Compaction of polymer • Entrapped air squeezed out via hopper • High pressure to control flow 3. Metering Zone • Melt homogenisation • Uniform flow at constant temperature and pressure
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14
Q

Briefly discuss the important features of the die design in the extrusion process.

A

The important features in die design are : • The adapter and die system must give a smooth flow of melt with no dead spots. • The approach channel to the final parallel should taper gradually to maintain compression and assist flow. • The die parallel must be long enough to exert back pressure to control uniform flow. • The die faces must be aligned precisely.

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15
Q

What is the purpose of the breaker plate and screen pack system on an extruder?

A

The breaker plate and screen pack system are supported by the adapter zone clamped against the barrel. The screen pack: 1. Acts as a filter for coarse particles and contaminants. 2. Creates a back-pressure without which control of the flow of the melt would not be possible; this flow control is essential for uniform production. The breaker plate serves the double function of: 1. Supporting the filter pack, and preventing the fine mesh wires breaking under the pressure developed in the melt by the screw. 2. Breaking up the rotational flow of the melt, converting it into translational flow into the adapter zone

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16
Q

How does melting take place in an extrusion process?

A
  1. Melting begins at the end of the feed zone. 2. Thin film of molten polymer forms at the barrel wall (heat source). 3. Advancing screw flight scrapes molten film off wall. 4. Melt pool accumulates in front of the advancing flight (high pressure side). 5. Solid bed accumulates behind advancing flight (low pressure side). 6. As material is transported downstream melt pool increases in size at the expense of the solid bed. 7. Melting should be completed before entering the metering zone. Melting takes place due to: 1. Transfer of heat from the barrel walls. 2. Dissipation of mechanical energy into heat through the deformation of the solid plastic.
17
Q

Discuss the effect of heating and cooling (fast and slow) in the polymer melt and the significance of these factors on the final product.

A

 Polymers are inherently poor conductors of heat, having very low thermal conductivities, and as such are vulnerable to localised overheating which can lead to degradation (chain scission). Most commercial polymers contain anti-oxidants to minimise this effect.  The removal of heat, i.e. the rate of cooling, will have a direct bearing on the structure and crystallinity of the product. In turn, these can influence the mechanical properties, the elastic recovery and shrinkage potential both during processing and in-service.  Too much heat will degrade the material. Too slow a removal of heat will result in a highly crystalline structure, which will be difficult to process subsequently.

18
Q

(a) Identify the major components of an injection-moulding machine. (b) Discuss the effect and type of defects in injected moulded parts.

A

(a). Material is fed into a heated barrel, mixed, and forced into a mold cavity where it cools and hardens to the configuration of the cavity. Injection moulding machine consists of two major components: Injection unit The mould assembly and clamping unit (b) Shrinkage and mould defects  Short shots – polymer solidification prior to the mould being filled.  Flashing – excess polymer squeezed out at the parting line in the tool.  Sink marks and voids – for thick mould sections because of the specific volume change during cooling if the solidified skin is thin then the internal stresses cause the surface to deflect causing a depression on the mould surface to accommodate the volume change. On the other hand if the skin is stiff and resists deflection then the volume change due to cooling must be accommodated internally and hence voids are formed.  Weld lines – when polymer is injected into a mould at more than one point a number of flow fronts move throughout the cavity until ultimately these meet up. The flow fronts on confrontation move transversely (parallel) to each other with no mass flow across the boundary forming a weakness between the two fronts. Under load this can be readily fractured. Careful component and tool design is required to ensure that this is not situated in a critical part of the component.

19
Q

Discuss the moulding assembly and clamping arrangement for an injection moulder.

A

Mould assembly is made up of at least two platens, which support the precision- engineered tool (mould). One half of this is movable so that the mould can be opened and closed to eject the solidified mouldings (components). The clamping unit can be toggle, hydraulic or hydromechanical mechanisms providing high pressures to resist the high injection pressures associated with this process, keeping the mould closed so that flash free components can be produced which require minimum trimming after ejection.

20
Q

Discuss how defects occur during the injection moulding process

A

 Short shots – polymer solidification prior to the mould being filled.  Flashing – excess polymer squeezed out at the parting line in the tool.  Sink marks and voids – for thick mould sections because of the specific volume change during cooling if the solidified skin is thin then the internal stresses cause the surface to deflect causing a depression on the mould surface to accommodate the volume change. On the other hand if the skin is stiff and resists deflection then the volume change due to cooling must be accommodated internally and hence voids are formed.  Weld lines – when polymer is injected into a mould at more than one point a number of flow fronts move throughout the cavity until ultimately these meet up. The flow fronts on confrontation move transversely (parallel) to each other with no mass flow across the boundary forming a weakness between the two fronts. Under load this can be readily fractured. Careful component and tool design is required to ensure that this is not situated in a critical part of the component.

21
Q

What are the three types of composites? – Give examples of each.

A
  1. Particulate: Concrete, cemented carbide (tungsten carbide particles in cobalt) 2. Fibrous: Wood, bone, glass fibre reinforced polymer, carbon fibre reinforced polymer 3. Laminate: Plywood
22
Q

What is the definition of a composite material?

A

 A composite material can be defined as: “A material system comprised of two or more physically distinct phases whose combination produces aggregate properties which are different and indeed superior to its constituents.”

23
Q

What is the role of the textile in a composite material?

A

 Textile reinforcements using engineering fibres for composites have good tensile strength and are lightweight but have poor performance in terms of compression or stiffness.  This necessitates the use of a matrix to encapsulate the fibres, thus:  Protecting them from damage (mechanical and/or environmental)  Enhancing the performance of the composite, in particular overcoming some of the weaknesses of textiles.

24
Q

What is the definition of a structural composite?

A

Structural composites can be defined as products which:  Use fibre reinforcements; e.g. carbon, aramid or glass, 50-70% by weight  Very high strength and stiffness  Made with polymeric metal and other matrices The matrix binds the reinforcing fibres together, forming a cohesive structure. Applied stresses transferred from one filament through the matrix to the adjacent filament. Polymeric matrices give low densities with very high specific properties i.e. high strength/weight and high stiffness/weight ratios.

25
Describe the nature of a composite material. Include in your answer comments on the properties of the constituent parts, the role of the constituent parts and the overall reasons for their use in engineering applications.
Fibres: Tensile Strength Weight It is of significance to note that in terms of strength, small deviations in fibre orientation lead to significant reductions in both tensile strength and tensile modulus. Matrix material: High temperature performance Transverse strength Moisture resistance Toughness Shear strength and in particular inter-laminar shear stress resistance (ILSS) Oxidation and radiation resistance.
26
Suggest 3 applications for composite materials and in each case include the following in your answer. Materials making up the composites Properties of the composite material that make it applicable to the suggested use. Processing method for the composite.
Boat manufacture Formula 1 Aircraft Each of these utilise the different materials in order to obtain the necessary physical/mechanical properties.
27
Briefly discuss how and why preimpregnated materials are used in advanced composite manufacture
Preimpregnated (prepreg) composites are the most prevalent product form used in advanced composite manufacturing. Prepregs typically consist of composite reinforcements (fiberglass, carbon fiber, aramid, etc.) that are embedded within a B-stage (partially cured) resin. • Limitations of producing high performance composite materials lies in the difficulty of achieving uniformity of fibre/resin distribution with low void content, using prepregs can help overcome this. • Controlled pre-impregnation using dip coating and lick roll technology to apply a uniform amount of uncured resin to the reinforcement is used to impregnate the reinforcement. • The resin contains both the base matrix resin and the hardeners in a B-staged resin system. The rolls of ‘prepreg’ are wrapped in release film and can be stored under refrigerated conditions for a period of time before the shelf-life of the product expires (normally 90 days at -18 0 C for aerospace quality materials). Advantages: Uniformity of resin distribution in the reinforcement. Eliminates the need for the processor to handle resin systems. Ease of use Disadvantages: Low temperature storage facilities are required. Finite shelf life.
28
a) Describe the manufacturing steps for the use of preimpregnated material and vacuum bagging system. b) What are the advantages of this type of manufacture?
• Plies of thawed out and conditioned prepreg are cut into the appropriate shape either by hand or an automated process. • Plies are placed in a precise order and orientation on a tool surface - critical to the performance of the composite. • A layer of release film is laid on top of the ply lay-up to prevent the resinous stack of plies from adhering to the fibrous breather cloth, which absorbs any excess resin and distributes the applied pressure evenly over the lay-up. • The complete assembly is enclosed in a sealed bag. • The ply stack is consolidated under approximately 1 Bar (100 kPa) of vacuum. • This complete assembly, while still under vacuum, is placed in an oven at an elevated temperature to cure the resin system Advantages: • Cost effective manufacture for non-structural components. • Can utilise room temperature prepreg. • Relatively low material and equipment costs. Disadvantages: • While this route uses prepreg material, which should ensure an even distribution of resin throughout the reinforcement, it is only operated at a maximum of approximately 1 Bar to consolidate the plies into a ‘homogeneous’ layer. • Low temperature storage required for prepreg. • Wastage of high value materials during ply cut-out (gerber cutter). • Health and safety precautions due to handling of prepreg.
29
Describe the steps involved in the manufacture of high structural composites by use of autoclave and prepreg technology.
 The plies are hand laid into the thoroughly degreased and clean moulding tool in the correct sequence and orientation. Constant inspection and signing-off of the lay-up at each stage is necessary to ensure performance and quality.  Where the component is comprised of a large number of plies frequent de-baulking is required i.e. the lay-up is compressed under vacuum, after which a further series of plies are laid-in.  A balanced lay-up, i.e. symmetry of lay-up about the neutral axis, minimises the extent of spring-back. Once the lay-up is completed, a layer of release film is placed on top of the plies, breather cloth placed on top of the release film and the whole assembly is bagged and sealed as shown.  Vacuum is then applied to the complete assembly.  After confirming the integrity of the seal, the bagged assembly while still under vacuum, is placed in a computer controlled autoclave which is programmed to follow a particular processing cycle of both temperature and pressure.
30
What are the advantages and disadvantages of the autoclave prepreg manufacturing process?
Advantages: • High fibre volume fraction, (60%) - quality composite • Low void content (\< 1%) - quality composite • Uniform fibre and resin distribution (controlled) • High performance Disadvantages: • Low temperature storage required for prepreg. • Wastage of high value materials during ply cut-out (gerber cutter). • Labour intensive and regular inspection required during ply lay-up. • Health and safety precautions due to handling of prepreg • Bottleneck in composite production
31
Discuss the use of preforms in the autoclave composite manufacture, rather than using prepreg, and relate the different processing steps including advantages over the use of prepreg.
Advantages: • Eliminate the need for cold storage, cutting and hand lay-up. • Less labour intensive. • Less costly.
32
Briefly discuss the advantages of using vacuum assistance and liquid moulding technology for production of high performance composites.
Resin impregnation under pressure has its performance limitations, but by using vacuum assistance first of all to evacuate the cavity and then to draw the degassed resin into the reinforcement, high performance composites can be produced. Advantages:  Low capital investment although mould costs may be higher is matched tooling is used.  Cold storage areas are not necessary and hence high value added products are not held in stock.  Shelf-life constraints are eliminated.  When preforms are used expensive cutting out and wastage are minimised and labour intensive hand lay-up is dispensed with. There may be some restrictions on the level of pressure which can be applied and hence the degree of consolidation of the composite.
33
Describe the different flow methodologies for introducing resin into the mould by liquid moulding vacuum assisted injection.
Investigations into different combinations of gating and pressure/vacuum injection have shown that peripheral gating and vacuum injection provide the most effective route to achieve this aim. Under this arrangement, the flow surrounds the reinforcement and then the flow front converges towards the vacuum exit point. The position of this is not critical since initial vacuum removing all the air from the sealed tool permits the in-flow of resin throughout the reinforcement. The progression of the fill of a rectangular plaque with the exit point deliberately off-set. Hence under these circumstances, venting, if at all necessary, is much less critical. Alternative injection method: Radial injection – whereby the resin is injected in the centre and the vacuum at the edge. There can be issues with the creation of resin starved areas by this method.
34
What are the advantages and disadvantages of composite manufacture by liquid moulding?
Advantages: • Low capital investment although may be complex (expensive) • Dry preforms used -- no cold storage required • Shelf-life constraints are not relevant • Near net-shaped preforms eliminate wasteful cutting out • Preforms laid into tool -- no handling of plies Disadvantages: • Lower pressures • Poorer consolidation
35
Discuss the process of resin film infusion.
To overcome the time-consuming process of de-aerating the resin system to ensure void-free composite manufacture, layers of resin in film form are laid into the ply assembly. When heated and pressure and/or vacuum is applied the resin becomes less viscous and flows to completely fill the interstices in the reinforcement and the spaces between the filaments. This is a much more rapid method and can be used for mass production of components. Even when complex three-dimensional reinforcements are used, resin film layers can be placed on the top and bottom surfaces, allowing resin, when heated, to be drawn throughout the reinforcement by vacuum.
36
Discuss the process of pultrusion.
• The basic process usually involves pulling of continuous fibers through a bath of resin, and then into pre-forming fixtures where the section is partially pre-shaped & excess resin is removed. It is then passed through a heated die, which determines the sectional geometry and finish of the final product. • This process produces I-beams or hollow rectangular tubes of uniform section and can be used in construction applications.
37
Why are ceramics useful for engineering applications?
Ceramics are useful for engineering applications due to their: high hardness, good electrical and thermal insulating characteristics, chemical stability and high temperature performance. In general they are brittle with little or no ductility which as with other materials causes difficulties in processing and performance of ceramic products.
38
Discuss the mechanical and physical properties of ceramics and how this relates to atomic arrangement.
Ceramic materials are rigid and brittle showing a perfectly elastic stress-strain characteristic. Ceramics in general have high elastic modulus and hardness particularly those based on non-silicates such as oxides and carbides. The covalent and ionic bonding makes ceramics quite strong, however unlike metals (metallic bonding) ceramic structures do not permit slip and hence they lack any plastic deformation and hence ductility under high stress. Therefore ceramics find difficulty in absorbing stress despite having vacancies, interstitial sites, displaced atoms and microscopic cracks. These internal flaws concentrate stresses, with brittle failure following when under tensile, flexural or impact loading. This results in relatively low tensile strengths and toughness. Ceramic materials are characterised by the covalent and ionic bonding (stronger than metallic bonding). These bonds account for the low ductility and high hardness of ceramics. Due to the tightly held electrons in the ceramic molecules ceramics are poor conductors of heat and electricity. The strong bonds give ceramics high melting temperatures with some decomposing rather than softening and melting. Ceramics usually adopt complex crystalline structures due to the presence of a number of different sized atoms in each molecule (SiO2 or Al2O3) and also consist of several elements (Al2Si2O5(OH)4). Some ceramics have an amorphous structure or glassy phase eg glass which consist primarily of fused silica.
39
What efforts can be made to minimise surface and internal flaws in ceramics?
Development of purer materials at the outset (fewer flaws) Decreasing grain size in the crystalline structure of products Minimising porosity Introducing compressive stresses eg glazing of surfaces Using fibre reinforcements Using heat treatments particularly quenching.